You limited your search to:

  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1952
 Serial/Series Title: NACA Technical Notes
 Collection: National Advisory Committee for Aeronautics Collection
Abnormal grain growth in S-816 alloy

Abnormal grain growth in S-816 alloy

Date: April 1952
Creator: Rush, A I; Freeman, J W & White, A E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Accuracy of approximate methods for predicting pressures on pointed nonlifting bodies of revolution in supersonic flow

Accuracy of approximate methods for predicting pressures on pointed nonlifting bodies of revolution in supersonic flow

Date: August 1952
Creator: Ehret, Dorris M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Achievement of continuous wall curvature in design of two-dimensional symmetrical supersonic nozzles

Achievement of continuous wall curvature in design of two-dimensional symmetrical supersonic nozzles

Date: January 1952
Creator: Evvard, J C & Marcus, Lawrence R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes

Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes

Date: June 1, 1952
Creator: Riebe, John M & Naeseth, Rodger L
Description: An investigation was made in the Langley 300-mph 7- by 10-foot tunnel to determine the aerodynamic characteristics of a refined deep-step planing-tail hull with various forebody and afterbody shapes and, for comparison, a streamline body simulating the fuselage of a modern transport airplane. The results of the tests indicated that the configurations incorporating a forebody with a length-beam ratio of 7 had lower minimum drag coefficients than the configurations incorporating a forebody with length-beam ratio of 5. The lowest minimum drag coefficients, which were considerably less than that of a conventional hull and slightly less than that of a streamline body, were obtained on the length-beam-ratio-7 forebody, alone and with round center boom. Drag coefficients and longitudinal- and lateral-stability parameters presented include the interference of a 21-percent-thick support wing.
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of three deep-step planing-tail flying-boat hulls and a transverse-step hull with extended afterbody

Aerodynamic characteristics of three deep-step planing-tail flying-boat hulls and a transverse-step hull with extended afterbody

Date: August 1, 1952
Creator: Riebe, John M & Naeseth, Rodger L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section

The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section

Date: June 1, 1952
Creator: Beckwith, Ivan E; Ridyard, Herbert W & Cromer, Nancy
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The aerodynamic design of supersonic propellers from structural considerations

The aerodynamic design of supersonic propellers from structural considerations

Date: December 1, 1952
Creator: Hammack, Jerome B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range

Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range

Date: September 17, 1952
Creator: Chapman, Dean R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analogue-computer simulation of an autopilot servo system having nonlinear response characteristics

Analogue-computer simulation of an autopilot servo system having nonlinear response characteristics

Date: June 1, 1952
Creator: Jones, Arthur L & White, John S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of flow in a subsonic mixed-flow impeller

Analysis of flow in a subsonic mixed-flow impeller

Date: August 1, 1952
Creator: Wu, Chung-Hua; Brown, Curtis A & Costilow, Eleanor L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of laminar free-convection flow and heat transfer about a flat plate parallel to the direction of the generating body force

An analysis of laminar free-convection flow and heat transfer about a flat plate parallel to the direction of the generating body force

Date: February 1, 1952
Creator: Ostrach, Simon
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of Landing-Gear Behavior

Analysis of Landing-Gear Behavior

Date: August 1, 1952
Creator: Milwitzky, Benjamin & Cook, Francis E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of normal accelerations and airspeeds of one type of twin-engine transport airplane in commercial operations over a northern transcontinental route

An analysis of normal accelerations and airspeeds of one type of twin-engine transport airplane in commercial operations over a northern transcontinental route

Date: November 1, 1952
Creator: Steiner, Roy
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of supersonic flow in the region of the leading edge of curved airfoils, including charts for determining surface-pressure gradient and shock-wave curvature

An analysis of supersonic flow in the region of the leading edge of curved airfoils, including charts for determining surface-pressure gradient and shock-wave curvature

Date: June 1, 1952
Creator: Kraus, Samuel
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of the errors in curve-fitting problems with an application to the calculation of stability parameters from flight data

An analysis of the errors in curve-fitting problems with an application to the calculation of stability parameters from flight data

Date: November 1, 1952
Creator: Shinbrot, Marvin
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of the normal accelerations and airspeeds of a two-engine type of transport airplane in commercial operations on routes in the central United States from 1948 to 1950

An analysis of the normal accelerations and airspeeds of a two-engine type of transport airplane in commercial operations on routes in the central United States from 1948 to 1950

Date: July 1, 1952
Creator: Walker, Walter G & Schumacher, Paul W J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical and experimental investigation of fully developed turbulent flow of air in a smooth tube with heat transfer with variable fluid properties

Analytical and experimental investigation of fully developed turbulent flow of air in a smooth tube with heat transfer with variable fluid properties

Date: February 1, 1952
Creator: Deissler, R G & Eian, C S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Application of linear analysis to an experimental investigation of a turbojet engine with proportional speed control

Application of linear analysis to an experimental investigation of a turbojet engine with proportional speed control

Date: February 1, 1952
Creator: Dandois, Marcel & Novik, David
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The application of planing characteristics to the calculation of the water-landing loads and motions of seaplanes of arbitrary constant cross section

The application of planing characteristics to the calculation of the water-landing loads and motions of seaplanes of arbitrary constant cross section

Date: November 1, 1952
Creator: Smiley, Robert F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Application of transonic similarity

Application of transonic similarity

Date: April 1, 1952
Creator: Busemann, Adolf
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An approach to the prediction of the frequency distribution of gust loads on airplanes in normal operations

An approach to the prediction of the frequency distribution of gust loads on airplanes in normal operations

Date: April 1, 1952
Creator: Press, Harry
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An approximate method for determining the displacement effects and viscous drag of laminar boundary layers in two-dimensional hypersonic flow

An approximate method for determining the displacement effects and viscous drag of laminar boundary layers in two-dimensional hypersonic flow

Date: September 1, 1952
Creator: Bertram, Mitchel H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An approximate method of determining the subsonic flow in an arbitrary stream filament of revolution cut by arbitrary turbomachine blades

An approximate method of determining the subsonic flow in an arbitrary stream filament of revolution cut by arbitrary turbomachine blades

Date: June 1, 1952
Creator: Wu, Chung-Hua; Brown, Curtis A & Prian, Vasily D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Approximate theory for calculation of lift of bodies, afterbodies, and combinations of bodies

Approximate theory for calculation of lift of bodies, afterbodies, and combinations of bodies

Date: April 1, 1952
Creator: Moskowitz, Barry
Description: None
Contributing Partner: UNT Libraries Government Documents Department
FIRST PREV 1 2 3 4 5 NEXT LAST